Two-phase heat transfer system including a thermal capacitance device

ABSTRACT

A two-phase heat transfer system includes an evaporator unit configured to receive heat from a source, a liquid line fluidly connected to the evaporator unit, a vapor line fluidly connected to the evaporator unit, and a condenser. The evaporation unit includes a thermal capacitance device and an evaporator integrated with the thermal capacitance device.

CROSS REFERENCE CROSS-REFERENCE TO RELATED APPLICATION

This application claims the benefit of U.S. Provisional Application No.60/655,485, filed Feb. 23, 2005, which is incorporated herein byreference in its entirety.

TECHNICAL FIELD

This description relates to a two-phase heat transfer system including athermal capacitance device.

BACKGROUND

Heat transfer systems are used to transport heat from one location (theheat source) to another location (the heat sink). Heat transfer systemscan be used in terrestrial or non-terrestrial applications. For example,heat transfer systems can be used in electronic equipment, which oftenrequire cooling during operation. Heat transfer systems can also be usedin, and integrated with satellite equipment that operates within zero orlow-gravity environments.

Loop Heat Pipes (LHPs) and Capillary Pumped Loops (CPLs) are examples ofpassive two-phase loop heat transfer systems. Each includes anevaporator thermally coupled to the heat source, a condenser thermallycoupled to the heat sink, fluid that flows between the evaporator andthe condenser, and a fluid reservoir for heat transfer systemtemperature control and for accommodating redistribution or volumechanges of the fluid. The fluid within the heat transfer system can bereferred to as the working fluid. The evaporator includes a primary wickand a core that includes a fluid flow passage. Heat acquired by theevaporator is transported to and rejected by the condenser. Thesesystems utilize capillary pressure developed in a fine-pored wick withinthe evaporator to promote circulation of working fluid from theevaporator to the condenser and back to the evaporator.

SUMMARY

In one general aspect, a two-phase heat transfer system includes anevaporator configured to receive heat from a source, a liquid linefluidly connected to the evaporator, a vapor line fluidly connected tothe evaporator, and a condensing unit. The condensing unit includes athermal capacitance device and a condenser thermally integrated with acondenser side of the thermal capacitance device. The condenser includesa vapor inlet fluidly connected to the vapor line and a liquid outletfluidly connected to the liquid line.

Implementations may include one or more of the following aspects. Forexample, the condensing unit may include a heat sink thermally connectedto a heat sink side of the condenser. The thermal capacitance device mayinclude a thermal storage unit. The thermal storage unit may include acore that defines channels for receiving a phase change material. Thethermal storage unit may include an end piece that surrounds a corefilled with phase change material. The condenser may include a condenserline that is thermally attached to an outer surface of the end piece.The condenser may include a condenser line that is defined within holesof the end piece, and the holes may be fluidly connected to the vaporinlet and the liquid outlet of the condenser. The thermal storage unitmay include a metallurgical bond between the core and the end piece. Thethermal capacitance device may define holes of the condenser that arefluidly connected to the vapor inlet and the liquid outlet.

In another general aspect, a two-phase heat transfer system includes acondenser configured to condense vapor, a liquid line fluidly connectedto the condenser, a vapor line fluidly connected to the condenser, andan evaporating unit. The evaporating unit includes an evaporator fluidlyconnected to the liquid line and to the vapor line and configured toreceive heat from a heat source. The evaporating unit includes a thermalcapacitance device integrated with the evaporator.

Implementations may include one or more of the following aspects. Forexample, the thermal capacitance device may include a thermal storageunit. The thermal storage unit may include a block that defines channelsfor receiving a phase change material. The block may surround theevaporator. The channels may feed into a plenum that is fluidly coupledto each of the channels. The thermal storage unit may include end capsthat seal to the block to maintain the phase change material within thechannels and the plenum. The thermal capacitance device may surround theevaporator.

In another general aspect, a method of forming a thermal storage unitincludes preparing a honeycomb core to receive a phase change material,metallurgically bonding both end pieces to the core to thermally linkthe end pieces to the core, and bonding the end pieces together to forma seal for holding the phase change material within the core.

Implementations may include one or more of the following aspects. Forexample, metallurgically bonding both end pieces to the core may includemetallurgically bonding one end piece to the core simultaneously withmetallurgically bonding the other end piece to the core. Bonding the endpieces together may include mating peripheral flanges on the end piecestogether using a seal weld. Bonding the end pieces together may includefastening the peripheral flanges together at a thick walled sectionaround a periphery of the end pieces.

Metallurgically bonding the end pieces to the core may include matingthe core and the end pieces, applying a solder to mating surfaces of theend pieces and/or the core, and heating the core, the end pieces, or thecore and the end pieces to melt the solder to bond the end pieces to thecore. The method may include cooling the end pieces and the core afterheating.

Metallurgically bonding the end pieces to the core may include bondingwithout the use of a flux. Metallurgically bonding the end pieces to thecore may include bonding without the use of a surface treatment on theend pieces or the core.

The method may include filling the core with the phase change material.

Other features and advantages will be apparent from the description, thedrawings, and the claims.

DESCRIPTION OF DRAWINGS

FIG. 1 is a perspective view of a thermal storage unit;

FIG. 2 is a cross-sectional view of a temperature-sensitive systemthermally coupled to the thermal storage unit of FIG. 1;

FIG. 3A is a schematic diagram of a two-phase heat transfer system;

FIG. 3B is a side cross-sectional view of a cylindrical evaporator thatcan be used in the heat transfer system of FIG. 3A;

FIG. 3C is a cross-sectional view of the evaporator of FIG. 3B takenalong section line 3C-3C;

FIG. 3D is a cross-sectional view of a flat evaporator that can be usedin the heat transfer system of FIG. 3A;

FIG. 4 is a schematic diagram of a two-phase heat transfer systemincluding a thermal capacitance condensing unit;

FIG. 5 is a perspective view of the condensing unit of FIG. 4;

FIG. 6 is a side plan view of the condensing unit of FIG. 5 showing theside that receives the cooling sink;

FIG. 7 is a side plan view of the condensing unit of FIG. 5 showing theside that receives a condenser;

FIG. 8 is a side plan view of the condensing unit of FIG. 5 taken alongsection line 8-8 of FIG. 7;

FIG. 9 is a cross-sectional view of the condensing unit of FIG. 5 takenalong section line 9-9 of FIG. 7;

FIG. 10 is a cutaway perspective view of a portion of the condensingunit of FIG. 5;

FIG. 11 is a flow chart of a procedure for manufacturing the condensingunit of FIG. 5;

FIG. 12 is a flow chart of a procedure for linking a core to end piecesof the condensing unit of FIG. 5;

FIG. 13 is a schematic diagram of a two-phase heat transfer systemincluding a thermal capacitance evaporating unit;

FIG. 14 is a center cross-sectional view of the evaporating unit of FIG.13;

FIG. 15 is a cross-sectional view of the evaporating unit of FIG. 14taken along section line 15-15 of FIG. 14; and

FIG. 16 is a cross-sectional view of another implementation of acondensing unit that can be used in the heat transfer system of FIG. 4.

Like reference symbols in the various drawings indicate like elements.

DETAILED DESCRIPTION

A thermal capacitance device is designed to reduce or minimize thetemperature fluctuations of a temperature-sensitive system that issubjected to temporally varying heat loads. The temperature-sensitivesystem can be a single component or a group of interrelated components.Referring to FIGS. 1 and 2, the thermal capacitance device may be athermal storage unit (TSU) 100 that reduces or minimizes temperaturefluctuations of a temperature-sensitive system 105 in a passive manner.As shown, the TSU 100 is a “latent heat” or isothermal TSU that changesphase to store heat. The latent heat TSU 100 is designed as a sealedvessel having a thermally conductive porous core 110 and a shell 115surrounding the core 110 and defining a void volume that houses the core110. The shell 115 and the core 110 are bonded at an interface 117. Thevoid volume in the core 110 is partially to nearly fully filled with aphase change material (PCM) that melts near an operating temperature ofthe system 105.

The shell 115 is made of two pieces 120, 125 that mate at an interface130 to form a hermetic seal for housing the PCM. The shell 115 is madeof a thermally conductive material to enable transfer of heat from thesystem 105 to the TSU 100. The system 105 and the TSU 100 are thermallymated at interface 135 between the piece 120 and the system 105. Theinterface 135 is typically a flat interface and mating between the piece120 and the system 105 may occur, for example, through bolting, gluing(such as with epoxy), clamping, welding, brazing, soldering, ordiffusion bonding. A diffusion bonding process is described in U.S.application Ser. No. 09/434,507, filed Nov. 5, 1999, now U.S. Pat. No.7,163,121, issued Jan. 16, 2007, which is incorporated herein byreference in its entirety.

The design and performance of the TSU 100 is dependent on an energystorage capacity (E) and an allowable temperature change (ΔT) of thesystem 105. Moreover, the two parameters E and ΔT may be affected by arelative density (or volume fraction) of the core 100; a lineardimension (or length) of the core 110, where the linear dimension isparallel to a principal direction 140 of heat flow; a lateral dimension(or area) of the core 110, where the lateral dimension is perpendicularto the principal direction 140 of heat flow; and thermo-physicalproperties of the core 110 and the PCM within the core 110. Moreover,the surface area-to-volume ratio of the core 110 can impact the designof the TSU 100. In one implementation, this ratio is set high enough toensure that the thermal resistance for heat flow into and out of the PCMcan be neglected.

Referring to FIG. 3A, a two-phase heat transfer system 300 thermallytransports heat from a heat source 305 using the capillary pressuredeveloped in a wick of a fine pore evaporator 310 to circulate a workingfluid within a closed loop. The heat transfer system 300 includes acondenser 315, a cooling sink 320 thermally coupled to the condenser 315at an interface 317, a fluid reservoir 325, a vapor line 330 from theevaporator 310 to the condenser 315, a liquid line 335 from thecondenser 315 to the evaporator 310, and a sweepage line 340 from theevaporator 310 to the reservoir 325. The fluid reservoir 325 may be coldbiased by a thermal connection 329 with the condenser 315. Additionally,the fluid reservoir 325 is in fluid communication with the vapor line330 by way of a reservoir line 327.

The cooling sink 320 is typically thermally coupled to the condenser 315by mounting the cooling sink 320 to a side of the condenser 315 toensure an efficient transfer of heat at the interface 317 between thecondenser 315 and the cooling sink 320. The evaporator 310 may be anydesign or shape suitable for thermally coupling to the heat source 305.Referring to FIGS. 3B and 3C, for example, the evaporator 310 can be acylindrical evaporator 350. In this case, the evaporator 350 includes acontainer 351 that houses a primary wick 352, within which a core 353 isdefined. The evaporator 350 may optionally include a bayonet tube 354and a secondary wick 355 within the core 353 and surrounding the bayonettube 354. The bayonet tube 354, the primary wick 352, and the secondarywick 355 define a liquid passage 360 and a vapor passage 362. Thesecondary wick 355 provides phase control, that is, liquid/vaporseparation in the core 353, as discussed in U.S. Pat. No. 6,889,754,issued May 10, 2005, which is incorporated herein by reference in itsentirety. Referring to FIG. 3D, as another example, the evaporator 310can be a flat plate evaporator 380, as described in U.S. Pat. No.6,915,843, issued Jul. 12, 2005, which is incorporated herein byreference in its entirety.

In operation, heat is acquired from the heat source 305 throughevaporation within the wick of the evaporator 310, vapor from theevaporator 310 flows out of the evaporator 310 through the internalvapor passage and through the vapor line 330 to the condenser 315, wherethe heat is rejected through condensation of the vapor into condensedliquid. The condensed liquid flows through the liquid line 335 and intothe liquid passage of the evaporator 310 to feed the wick of theevaporator 310, where it is available for evaporation. Moreover, vaporand/or bubbles of non-condensable gas (NCG bubbles) are vented from acore of the evaporator 310 through the sweepage line 340 and into thereservoir 325. Additionally, fluid, from the reservoir 325 can be drawninto the condenser 315 through the reservoir line 327.

Two-phase heat transfer systems have no moving parts and are passive(and are, therefore, generally reliable). They can be used for variousapplications including spacecraft thermal control. For example,spacecraft waste heat may be transported by a two-phase heat transfersystem to its condenser (a space-facing radiator). Two-phase heattransfer systems can be miniaturized and can be utilized to cool avariety of heat dissipating components including components that operateat cryogenic temperatures.

The two-phase heat transfer system 300 is formed by thermally attachingthe evaporator 310 to the heat source 305, routing the fluid lines 330,335 from the evaporator 310 to the condenser 315, thermally attachingthe condenser 315 to the cooling sink 320, and controlling thetemperature of the reservoir 325 for variable loop conductance andtemperature stability of the heat source 305. The condenser 315 mayinclude either a single channel or multiple-parallel channels that aremade of smooth-walled tubing. The size, the length, and the number ofchannels affect the heat transfer area and the pressure drop. As thecross-sectional area of a channel is reduced, the condensation filmcoefficient increases (reducing the required condenser area) but thepressure drop also increases. Increasing the number of channels ormaking the channels shorter can offset this pressure drop, butmanufacturing limitations may arise as the channel size is reduced andmore complex methods are needed.

Referring to FIG. 4, a two-phase heat transfer system 400 includes acondensing unit 415 that includes a thermal capacitance deviceintegrated with a condenser. The condensing unit 415 replaces the solecondenser 315 that is shown in the system 300 above. Like the heattransfer system 300 above, the heat transfer system 400 thermallytransports heat from a heat source 405 using the capillary pressuredeveloped in a wick of a fine pore evaporator 410 to circulate a workingfluid within a closed loop. In some applications, such as thoseapplications involving spacecraft, the temporal heat sources are locatedremotely from the cooling sink. In these cases, heat transport can beefficiently accomplished with a single-evaporator or a multi-evaporatortwo-phase heat transfer system. To enable the load-leveling benefits ofa thermal capacitance device to be afforded to all temporally varyingheat sources serviced by the (single- or multi-evaporator) two-phaseheat transfer system, the thermal capacitance device is thereforethermally linked to the condenser of the two-phase heat transfer systemto form the two-phase heat transfer system 400.

The heat transfer system 400 includes a heat sink 420 thermally coupledto the condensing unit 415, a fluid reservoir 425, a vapor line 430 fromthe evaporator 410 to the condensing unit 415, a liquid line 435 fromthe condensing unit 415 to the evaporator 410, and a sweepage line 440from the evaporator 410 to the reservoir 425. The fluid reservoir 425 isin fluid communication with the vapor line 430 by way of a reservoirline 427. The fluid reservoir 425 may be cold biased by a thermalconnection 429 with the condensing unit 415.

In operation, heat is acquired at the heat source 405 throughevaporation within the evaporator 410, vapor from the evaporator 410flows through the vapor line 430 to the condensing unit 415, where theheat is rejected through condensation of the vapor into condensedliquid. The condensed liquid flows through the liquid line 435 to theevaporator 410, where it is available for evaporation. Moreover, vaporand/or bubbles of non-condensable gas (NCG bubbles) can be vented from acore of the evaporator 410 through the sweepage line 440 and into thereservoir 425. Additional fluid, as needed, can be pulled from thereservoir 425 through the reservoir line 427 and into the condensingunit 415.

The condensing unit 415 is designed in a thermally efficient manner.Thus, the thermal capacitance device and the condenser within thecondensing unit 415 are in an integral assembly, as discussed below withrespect to FIGS. 5-10. Moreover, to achieve an integral assembly, thethermal capacitance device and the condenser are designed to begeometrically and thermally compatible to reduce thermal resistancebetween the thermal capacitance device and the condenser. The thermalcapacitance device is constructed in a manner that facilitates orenables attachment of the condenser lines (or tubing) of the condenserto the thermal capacitance device while maintaining the heat transferbetween the thermal capacitance device and the condenser.

Referring to FIGS. 5-10, the condensing unit 415 includes a thermalstorage unit (TSU) 500 and condenser lines 505 thermally coupled to andintegral with the thermal storage unit 500. The TSU 500 is constructedwith a core 510 sandwiched between two pan-shaped end pieces 515, 520.

The end piece 515 thermally couples to the condenser lines 505, whilethe end piece 520 acts a cold side of the TSU 500 and thermally couplesto the heat sink 420. The condenser lines 505 can be made of, forexample, an aluminum extrusion that includes a thin flange 507 that hasa flat surface that mates with the end piece 515. As shown, the heatsink 420 is designed as lines of chilled fluid 525 that are thermallycoupled to the end piece 520. The chilled fluid lines 525 can be madeof, for example, aluminum extrusion that includes a thin flange 527 thathas a flat surface that mates with the end piece 520.

Each end piece 515, 520 respectively includes a base 550, 555, and thickwalled section 560, 565 (as shown in FIGS. 9 and 10) directlysurrounding the periphery of the base 550, 555. Each end piece 515, 520respectively includes a peripheral flange 540, 545 that wraps around aperiphery of the base 550, 555 of the end piece 515, 520. The peripheralflanges 540, 545 extend from the base 550, 555 such that when the endpieces 515, 520 are mated, the flanges 540, 545 touch along an interface542, and the core 510 is held between the bases 550, 555 and inside thethick walled sections 560, 565.

Each end piece 515, 520 also includes fasteners 570 that are insertedthrough the thick walled sections 560, 565, respectively, to ensure thecondenser lines 5.05 and the chilled fluid lines 525, which are eachbonded on the respective bases 550, 555 of the condensing unit 415, donot delaminate. The fasteners 570 are shown as screws that are insertedinto throughholes of the flanges 507, 527 and into the thick walledsection of the end pieces 515, 520.

In one implementation, the core 510 is made of a honeycomb structurethat includes channels elongated along a core axis, where each channelhas a honeycomb (hexagonal cross-section) geometry taken along a sectionthat is perpendicular to the core axis. The PCM is received within thechannels. In other instances of this implementation, the channels havean effective cross-sectional size (or width) of less than or equal toabout 0.1″. The honeycomb structure of the core 510 can be partially tofully expanded prior to installation of the core 510 within the endpieces 515, 520. Thus, the geometry of the honeycomb structure of thecore 510 can be expanded to a particular density prior to installationwithin the end pieces 515, 520. The particular density of the honeycombstructure should be high enough so that the thermal resistance betweenthe core 510 and the PCM that fills the core 510 is reduced orminimized. In one implementation, the honeycomb structure is partiallyexpanded within the core 510, such that the width of the channel in thepartially expanded honeycomb structure is about one-fifth of the widthof a channel in a fully expanded honeycomb structure and such that thechannel relative density is about five times the density of a fullyexpanded honeycomb structure and about 10% of the density of a fullysolid core.

The core 510 is made of a material that is thermally conductive (forexample, having a thermal conductivity greater than about 100 W/mK) toprovide for a suitable transfer of heat between the end pieces 515, 520and the core 510. The core 510 is made from a material that isrelatively lightweight (for example, having a density less than about5000 kg/m³), that is machinable, that has moderate strength anddurability to withstand the volume change of the PCM during a phasechange, and that is able to be attached to the end pieces 515, 520. Forexample, the core 510 may be made of aluminum, copper, beryllium,molybdenum, beryllium copper, graphite, graphite foam, aluminum nitride,aluminum carbide, beryllium oxide, magnesium, tungsten, silver, gold,and zinc.

The end pieces 515, 520 are made of material that is thermallyconductive (for example, having a thermal conductivity greater thanabout 100 W/mK) to provide for a suitable transfer of heat between theend pieces 515, 520 and the condenser lines 505 or the radiator 420 andthe end pieces 515, 520 and the core 510. The end pieces 515, 520 aremade from a material that is relatively lightweight (for example, havinga density less than about 5000 kg/m³), that is machinable, that issealable (for example, to the core 510 or to the condenser lines 505 orthe radiator 420), and that has moderate strength and durability towithstand possible pressure changes. For example, the end pieces 515,520 may be made of aluminum, copper, beryllium, molybdenum, berylliumcopper, graphite, aluminum nitride, aluminum carbide, beryllium oxide,magnesium, tungsten, and zinc.

The use of the thermal capacitance device within the condensing unitreduces temperature fluctuations in a temperature-sensitive system thatis subjected to temporally varying heat loads. The use of the thermalcapacitance device, whether used in a stand-alone application or inconjunction with a two-phase heat transfer system reduces the need forlarger heat rejection subsystems (radiators).

The two-phase heat transfer system that includes a thermal capacitancecondensing unit can be better able (without increasing cooling systemsize/weight) to reduce the temperature fluctuations oftemperature-sensitive and two-phase heat transfer system cooledcomponents and systems subjected to temporally varying heat loads.Additionally, the condensing unit has good heat load scalability. Ingeneral, integrating the functionalities of a thermal capacitance devicewith a condenser of a two-phase heat transfer system results in asmaller-sized system and a compact heat rejection subsystem (radiator)sized for an average rather than a peak heat load. Thus, sizerequirements of the two-phase heat transfer system can be reduced, andthe temperature fluctuation of the heat source can be reduced.

Referring to FIG. 11, the condensing unit 415 is manufactured accordingto a process 1100. Initially, the core 510 is prepared (step 1105). Thecore 510 can be prepared by purchasing a pre-fabricated core fromAlcore, Inc. of Lakeside Business Park, 1502 Quarry Drive, Edgewood, Md.21040 USA. Such cores can be found at Alcore's website atwww.alcore.com. Next, the pre-fabricated core 510 is expanded to a sizesuitable for a requisite density and strength for joining with the endpieces 515, 520.

The end pieces 515, 520 are also fabricated (step 1110). The end pieces515, 520 can be fabricated by machining a block of material into theappropriate shape to form the peripheral flanges 540, 545 and the bases550, 555, respectively.

Next, the core 510 is thermally linked to the two end pieces 515, 520at, respectively, interfaces 530, 535 (shown in FIGS. 9 and 10) (step1115). The core 510 can be linked to the two end pieces 515, 520 usingany process that enables efficient transfer of heat between the core 510and the end pieces 515, 520. For example, the core 510 can be glued tothe end pieces 515, 520, or the core 510 can be pressed between the endpieces 515, 520.

In one implementation, the core 510 is thermally linked to the endpieces 515, 520 using a metallurgical bonding process. Referring to FIG.12, a procedure 1115 is performed to thermally link the core 510 to theend pieces 515, 520 using the metallurgical bonding process. Themetallurgical bonding process described herein provides good thermalconductivity between the core 510 and the end pieces 515, 520. Solder isapplied to each of the inner surfaces of the end pieces 515, 520 (at theinner surfaces that form the interfaces 530, 535) (step 1205). Solder isapplied without the use of flux and without the need to surface treatthe seam. The core 510 and both of the end pieces 515, 520 are matedtogether to form a seam at the interfaces 530, 535 (step 1210). Next,the core 510 and the end pieces 515, 520 are heated to a high enoughtemperature to melt the solder (step 1215) to enable the solder to bondthe core 510 to the end pieces 515, 520. The solder has a high enoughsurface tension such that the solder does not stick to the core 510during heating. In particular, the surface tension of the solder is highenough to prevent the channels within the honeycomb core 510 frombecoming filled with the solder during heating. Furthermore, themetallurgical bonding process uses a solder that has a high thermalconductivity to provide for suitable thermal conductivity between thecore 510 and the end pieces 515, 520. In one implementation, the endpieces 515, 520 are heated simultaneously to melt the solder applied toboth of the inner surfaces so that the bond can be formed simultaneouslyat both interfaces 530, 535. Next, after the solder is sufficientlyheated, the heat is removed and the core 510 and the end pieces 515, 520are permitted to cool (step 1220).

In one implementation, the metallurgical bonding process includes anS-BOND® process, which is implemented by S-Bond Technologies of 811 W.Fifth Street, Lansdale, Pa. 19446. More information on the S-BOND®process can be found at http://www.s-bond.com/s-bond/sbond.htm or fromS-Bond Technologies. The S-BOND® process is described in U.S. Pat. No.6,047,876, issued Apr. 11, 2000, which is incorporated herein byreference.

The end pieces 515, 520 and the core 510 are designed such that afterthe metallurgical bonding process, the mating peripheral flanges 540,545 on, respectively, the two end pieces 515,520 are close enough suchthat the flanges 540, 545 can be attached to each other.

Thus, after the core 510 is thermally linked to the end pieces 515, 520,the flanges 540, 545 are attached to join the end pieces 515, 520together (step 1120). In particular, the flanges 540, 545 can beattached by seal-welding the flanges 540, 545. In anotherimplementation, the flanges 540, 545 can be attached by diffusionbonding, or welding or brazing with or without the use of a filler metalor an adhesive. In a further implementation, the flanges 540, 545 can beattached using a hot isostatic pressure bond method, as described inU.S. Pat. No. 6,264,095, issued on Jul. 24, 2001, which is incorporatedherein by reference in its entirety. In one implementation, the flanges540, 545 can be attached by screwing the thick walled sections 560, 565down at each end using additional external clamping hardware to clampthe flanges 540, 545 together.

After the flanges 540, 545 are attached (step 1120), the PCM is added tothe core 510 to fill the void volume within the honeycomb structure ofthe core 510 (step 1125). The PCM may be added using any standard fillprocess through one or more tubes 575 that are coupled to opening alongsides of the end piece 515, 520. The opening can be located at one ofthe sides of the end piece 515, 520 through which the core axis passesso that the PCM can more easily flow into all of the channels(hexagonally shaped cells) of the core 510.

Next, the chilled fluid lines 525 are attached to the outer surface ofthe end piece 520 (step 1130). The fluid lines 525 can be attachedusing, for example, glue, epoxy, or any suitable film adhesive, or bybrazing or soldering. The condenser lines 505 are attached to the outersurface of the end pieces 515 (step 1135). The condenser lines 505 canbe attached using, for example, glue, epoxy, or any suitable filmadhesive, or by brazing or soldering.

The condensing unit 415 reduces the temperature fluctuation of atemperature-sensitive component subjected to a temporally varying heatsource 405, and minimizes the size and weight of the two-phase heattransfer system 400. For a temperature-sensitive heat source subjectedto a temporal heat load, one typical heat load profile of the condensingunit 415 is a peak heat load of Q_(MAX), which lasts for 10% of therecurring period, a minimum heat load of Q_(MAX)/9, which lasts for theremaining 90% of the recurring period. For such a typical duty cycle;the average heat load is about Q_(MAX)/5. An infinite number ofalternate heat load profiles are possible.

The two-phase heat transfer system 400 can be used in pulsed high powerand low duty cycle spacecraft instrument modules that are highlytemperature sensitive. And, by virtue of the small footprint of theinternal heat sources of these instrument modules, the pulsed high powerand low duty cycle spacecraft instrument module is suited to an internaltwo-phase heat transfer system. The pulsed high power and low duty cyclespacecraft instrument module uses the two-phase heat transfer system 400to prevent high peak loads from flowing into the spacecraft and toprevent excessive instrument module temperature fluctuations.

Other implementations are within the scope of the following claims.

For example, in another implementation, the TSU 100 can be a “sensibleheat” TSU that changes temperature to store heat. In thisimplementation, the sensible heat TSU includes a solid mass of high heatcapacity, thermally conductive material that changes temperature tostore heat.

For a space application, the end piece 520 that is attached to the coldside of the TSU can be thermally coupled to a space-facing radiator 420.

Referring to FIG. 13, a two-phase heat transfer system 1300 includes anevaporating unit 1310 that includes a thermal capacitance deviceintegrated with an evaporator. The evaporating unit 1310 replaces thesole evaporator 310 that is shown in the system 300 above. Like the heattransfer system 300 above, the heat transfer system 1300 thermallytransports heat from a heat source 1305 using the capillary pressuredeveloped in a wick of a fine pore evaporator of the evaporating unit1310 to circulate a working fluid within a closed loop. The heattransfer system 1300 includes a radiator 1320 thermally coupled to acondenser 1315, a fluid reservoir 1325, a vapor line 1330 from theevaporating unit 1310 to the condenser 1315, a liquid line 1335 from thecondenser 1315 to the evaporating unit 1310, and a sweepage line 1340from the evaporating unit 1310 to the reservoir 1325. The reservoir 1325is coupled to the vapor line 1330 through a reservoir line 1327.

Referring also to FIGS. 14 and 15, the evaporating unit 1310 is designedin a thermally efficient manner, in which the thermal capacitance deviceand the evaporator are in an integral assembly. Moreover, to achieve anintegral assembly, the thermal capacitance device and the evaporator aredesigned to be geometrically and thermally compatible to reduce thermalresistance between the thermal capacitance device and the evaporator.

As shown, the evaporating unit 1310 includes an evaporator 1400 insideof a thermal capacitance device in the form of a thermal storage unit1405. The thermal storage unit 1405 includes a block 1410 of materialsurrounding the evaporator 1400 and including a plurality of channels1415. Each of the channels 1415 feeds into a plenum 1420 formed withinand along at least one side of the block 1410. The thermal storage unit1405 includes an end cap 1425 that thermally bonds with the block 1410and fluidly seals the plenum 1420 and the channels 1415. The thermalstorage unit 1405 includes at least one fill port 1430 that feeds intothe plenum 1420. The fill port 1430 is attached to the end cap 1425 byan appropriate method, such as, for example, brazing or welding, toensure a seal between the fill port 1430 and the end cap 1425. The fillport 1430 can be hermetically sealed off by an appropriate method, suchas, for example, pinching or welding. The evaporating unit 1310 alsoincludes ports that feed into and out of the evaporator 1400, including,for example, a liquid inlet 1435 that feeds into the evaporator 1400 anda vapor outlet 1440 that feeds out of the evaporator 1400.

The block 1410 is made of a thermally conductive material to enabletransfer of heat throughout the block 1410. For example, the material ofthe block 1410 has a thermal conductivity greater than about 100 W/mK toprovide for a suitable transfer of heat between the block 1410 and theevaporator 1400 or the block 1410 and the PCM within the channels 1415.The block 1410 is made from a material that is relatively lightweight(for example, having a density less than about 5000 kg/m³), that ismachinable, that is sealable (for example, to the end caps 1425), and,that has moderate strength and durability to withstand possible pressurechanges. For example, the block 1410 may be made of aluminum, copper,beryllium, molybdenum, beryllium copper, graphite, aluminum nitride,aluminum carbide, beryllium oxide, magnesium, tungsten, and zinc. Theend caps 1425 are made of a material that is strong enough to withstandpossible pressure changes, is relatively lightweight, and is sealable,for example, to the block 1410. For example, the end caps 1425 may bemade of aluminum, copper, beryllium, molybdenum, beryllium copper,graphite, aluminum nitride, aluminum carbide, beryllium oxide,magnesium, tungsten, and zinc.

To prepare the evaporating unit 1310 for operation, the PCM isintroduced into the thermal storage unit 1405 through the fill port1430, such that the PCM that passes through the fill port 1430 entersthe plenum 1420 and the channels 1415. The PCM is able to pass freelythrough the plenum 1420 and the channels 1415. Next, the ports attachedto the evaporator 1400 are connected to the appropriate fluid lines ofthe heat transfer system 1300. For example, the liquid inlet 1435 isfluidly connected to the liquid line 1335 and the vapor outlet 1440 isfluidly connected to the vapor line 1330.

In operation, heat is acquired at the heat source 1305 throughevaporation within the evaporator of the evaporator unit 1310, vaporfrom the evaporator 1400 flows through the vapor outlet 1440, throughthe vapor line 1330 to the condenser 1315, where the heat is rejectedthrough condensation of the vapor into condensed liquid. The condensedliquid flows through the liquid line 1335, through the liquid inlet1435, and into the evaporator 1400, where it is available forevaporation. Moreover, vapor and/or bubbles of non-condensable gas (NCGbubbles) are vented from a core of the evaporator 1400 within theevaporator unit 1310 through the sweepage line 1340 and into thereservoir 1325.

Referring also to FIG. 16, in another implementation, the two-phase heattransfer system 400 can be designed with a condensing unit 1615 thatincludes a TSU 1700 integrated with a condenser 1705. In the condensingunit 1615, the condenser 1705 is provided as holes that are formed (forexample, by machining) through an end piece 1715 of the condensing unit1615. As shown in FIG. 16, the end piece 1720 is otherwise designed in asimilar manner to the end piece 520 described above. In particular, theTSU 1700 includes a core 1710 that is sandwiched between the twopan-shaped end pieces 1715, 1720. Each end piece 1715, 1720 respectivelyincludes a base 1750, 1755, and thick walled sections 1760, 1765directly surrounding the periphery of the base 1750, 1755. Each endpiece 1715, 1720 respectively includes a peripheral flange 1740, 1745that wraps around a periphery of the base 1750, 1755 of the end piece1715, 1720, much like the design of the flanges 540, 545 describedabove. Thus, the main difference between the condensing unit 1615 andthe condensing unit 415 is the location of the condenser 1705. In thecondensing unit 1615, the condenser 1705 is within the end piece 1715,while in the condensing unit 415, the condenser lines 505 are attachedto an outer surface of the end piece 515. In both cases, there is athermal connectivity between the PCM within the condenser 1705 orcondenser lines 505 and the end piece 1715 or 515, respectively.

It is also or alternatively possible to design the end piece 1720 in amanner in which the chilled fluid lines 1725 are inside of the end piece1720 much like the condenser 1705 is designed within the end piece 1715.

1. A two-phase heat transfer system comprising: a condenser configuredto condense vapor; a liquid line fluidly connected to the condenser; avapor line fluidly connected to the condenser; and an evaporating unitincluding: an evaporator fluidly connected to the liquid line and to thevapor line and configured to receive heat from a heat source, theevaporator comprising a core having a liquid passage formed therein; anda thermal capacitance device integrated with the evaporator, the thermalcapacitance device comprising a thermal storage unit including a blockhaving a plurality of channels formed therein, the plurality of channelsextending in a direction substantially parallel to the liquid passageformed in the core of the evaporator, and wherein a portion of the blockis in contact with a portion of the evaporator.
 2. The two-phase heattransfer system of claim 1, wherein each channel of the plurality ofchannels has a phase change material disposed therein.
 3. The two-phaseheat transfer system of claim 1, wherein the block surrounds theevaporator, an inner surface of the block contacting an outer surface ofthe evaporator.
 4. The two-phase heat transfer system of claim 1,wherein each channel of the plurality of channels feeds into a plenumthat is fluidly coupled to each of the channels.
 5. The two-phase heattransfer system of claim 4, wherein the thermal storage unit includesend caps that seal to the block to maintain the phase change materialwithin the channels and the plenum.
 6. The two-phase heat transfersystem of claim 1, wherein the plurality of channels formed in the blocksurround the evaporator.
 7. The two-phase heat transfer system of claim1, wherein the evaporating unit comprises a plurality of evaporatorunits, each evaporating unit comprising: an evaporator fluidly connectedto the liquid line and to the vapor line and configured to receive heatfrom a heat source; and a thermal capacitance device integrated with theevaporator.
 8. The two-phase heat transfer system of claim 1, whereinthe condenser comprises a thermal capacitance device, the condenserthermally coupled with a condenser side of the thermal capacitancedevice.
 9. The two-phase heat transfer system of claim 8, wherein thethermal capacitance device is disposed within the condenser.
 10. Thetwo-phase heat transfer system of claim 1, wherein the evaporatorcomprises a wick disposed within the core of the evaporator.
 11. Thetwo-phase heat transfer system of claim 10, wherein the evaporatorfurther comprises a secondary wick disposed within the core and the wickof the evaporator.
 12. The two-phase heat transfer system of claim 1,wherein the thermal storage unit comprises at least one plenum formedtherein adjacent to the block, each channel of the plurality of channelsformed in the block being in fluid communication with the at least oneplenum.
 13. The two-phase heat transfer system of claim 12, wherein theat least one plenum formed in the thermal storage unit comprises twoplenums formed in the thermal storage unit adjacent to opposing ends ofthe block, each channel of the plurality of channels formed in the blockbeing in fluid communication with each of the two plenums.